A method of welding two workpieces together is described. A conductor in electrical communication with a pulse circuit is provided. A portion of the second workpiece is located adjacent the conductor. The two workpieces are also located together. A portion, or all, of one workpiece is welded to the other by applying a pulse current to one of the workpieces. A method of forming a workpiece is disclosed using a pulse current to move the workpiece into a desired shape.
|
15. A method of welding workpieces together, comprising:
providing a first workpiece;
providing a second workpiece, the second workpiece having an embossed portion formed therein;
placing the first workpiece against the second workpiece so that the embossed portion extends from the first workpiece;
placing the embossed portion adjacent a conductor;
welding the embossed portion of the second workpiece to the first workpiece by applying a pulse current through the embossed portion;
restraining the first workpiece and the second workpiece against a restraining member.
1. A method of welding two workpieces together, comprising:
providing a first workpiece, the first workpiece being substantially flat;
providing a second workpiece, the second workpiece having a substantially flat portion and an embossed portion formed therein;
providing a conductor in electrical communication with a pulse circuit;
placing the embossed portion of the second workpiece adjacent the conductor, the second workpiece in electrical contact with the pulse circuit and the conductor;
abuttingly disposing the first workpiece against the substantially flat portion of the second workpiece;
welding the embossed portion of the second workpiece to the first workpiece by applying the pulse current to the second workpiece;
restraining the first workpiece and the second workpiece against a restraining member.
26. A method of forming a workpiece, comprising:
providing a first workpiece;
placing the first workpiece in direct contact a first electrical contact and placing the first workpiece in direct contact with a second electrical contact, said second electrical contact in electrical communication with a magnetic field generating portion;
applying a pulse current through said first electrical contact to travel through said first workpiece in a first direction to said second electrical contact;
creating a magnetic field by routing said pulse current in a second direction, opposite said first through said magnetic field generating portion;
forming said first workpiece into at least a portion of a restraining member located adjacent said first workpiece;
restraining the first workpiece and the second workpiece against said restraining member.
27. A method of attaching two workpieces, comprising:
providing a first non-planar workpiece;
providing a second non-planar workpiece;
locating a restraining member adjacent said first workpiece and said second workpiece to restrain said workpieces, said restraining member having a complimentary shape to said first workpiece;
locating a magnetic field generating portion adjacent said second workpiece, said magnetic field generating portion having a complimentary shape to said second workpiece;
positioning an insulator between said magnetic field generating portion and said second workpiece;
providing a first contact for delivering a pulse current through said second workpiece to a second contact in a first direction, said pulse current extending through said magnetic field generating portion in a second direction, opposite said first direction, to develop a magnetic field that drives said second workpiece into welded contact with at least a portion of said first workpiece.
2. The method of
3. The method of
4. The method of
5. The method of
6. The method of
7. The method of
8. The method of
10. The method of
11. The method of
12. The method of
13. The method of
14. The method of
16. The method of
17. The method of
18. The method of
19. The method of
21. The method of
22. The method of
23. The method of
24. The method of
25. The method of
|
This application claims priority to U.S. patent application Ser. No. 61/545,324 filed on Oct. 10, 2011 which is incorporated by reference in its entirety.
The present invention relates to magnetic pulse welding and forming and more specifically to using magnetic pulse welding to couple plates, such as battery plates, or using magnetic pulse forming to form plates.
There are a variety of methods for connecting plates together, such as plates for a battery. A common method of connecting the battery plates together is by welding. One type of welding that is used is ultrasonic welding. Ultrasonic welding is well-known, readily available and cost-effective, however, it has disadvantages, particularly for battery plates.
Often ultrasonic welding of battery plates results in significant deformation of one or more of the plates at the weld location when the weld is completed. This permanent deformation can damage or ruin the plates thus making them unusable or inefficient. Thus, a different method of connecting the plates together is needed that does not result in permanent damage to the connected plates.
There are also a variety of methods for forming plates, or portions of plates, into desired shapes. Presses and dies are frequently used but, depending on the desired shape, the cycle time to create the shape can be undesirable. Additionally, it can be difficult to create some shapes using presses/dies. Instead, it would be desirable to have a process for forming plates, or portions of plates, in a quick and accurate method.
A method of welding two workpieces together is provided. The method comprises providing a first workpiece and a second workpiece to be welded to the first. The second workpiece may have an embossed portion formed therein. A conductor is provided that is in electrical communication with a pulse circuit. Where an embossed portion of the second workpiece is provided, it is placed adjacent the conductor. The first workpiece is disposed against the second workpiece. A restraining member is located against one of the workpieces. A pulse current is applied to the second workpiece to weld it to the first workpiece.
A method for forming a portion of a workpiece is also disclosed using a pulse current. The method comprises providing a workpiece. The workpiece is located adjacent a conductor. The workpiece is also located adjacent a restraining member. The restraining member may have a desired shape formed therein. A pulse current is applied to the workpiece to form it against the restraining member shape.
The above, as well as other advantages of the present invention, will become readily apparent to those skilled in the art from the following detailed description when considered in the light of the accompanying drawings in which:
It is to be understood that the invention may assume various alternative orientations and step sequences, except where expressly specified to the contrary. It is also to be understood that the specific devices and processes illustrated in the attached drawings, and described in the following specification are simply exemplary embodiments of the inventive concepts defined herein. Hence, specific dimensions, directions or other physical characteristics relating to the embodiments disclosed are not to be considered as limiting, unless expressly stated otherwise.
The pulse welding system 10 includes a first terminal 16, a proximity conductor 18, a restraining member 20, and a pulse circuit 22. As shown in
While a work surface 24 is provided, the present invention works equally well without the surface. The work surface may support the components described herein, as suggested above, and/or it may function to house and enclose the components mentioned here as well as other components are not discussed.
As shown in
The first workpiece 12 may have a planar upper surface 12A and a planar lower surface 12B. The surfaces 12A, 12B may be separated from one another by a substantially constant thickness.
As shown in
The substantially flat portion 26 of the second workpiece 14 is a non-embossed portion of the second workpiece 14. As shown in
Except for the embossed portion 28, the second workpiece 14 may have a planar upper surface 14A and a planar lower surface 14B. The surfaces 14A, 14B may be separated from one another by a substantially constant thickness.
The embossed portion 28 may be formed by stamping the second workpiece 14 between a male die and a female die. As shown in
Additionally, the term “embossed portion” may refer to a portion of the second workpiece 14 that is not in fact formed by embossing. Instead, the portion may be formed by any known method of displacing one portion of a plate from another. Such methods include, but are not limited to, punching, stamping, cold forming and/or pressing.
The work surface 24 is preferably formed from a non-conductive material; however, it is understood that any material may be used, where the work surface 24 is electrically insulated from at least one of the first terminal 16 and the proximity conductor 18. The work surface 24 is substantially planar and includes a terminal aperture 30 formed therethrough. As shown in
The first terminal 16 is a conductor disposed in the terminal aperture 30 of the work surface 24. The first terminal 16 may be rigidly mounted with respect to the work surface 24 using any conventional coupling means. As mentioned hereinabove, the first terminal 16 is preferably electrically insulated from the work surface 24.
The first terminal 16 may be a hollow cylinder and has a contact end 32 and a circuit end 34; however, it is understood the first terminal 16 may be any other shape, such as a rectangular elongate member. Preferably, the first terminal 16 is continuous and unitary from the contact end 32 to the circuit end 34.
Except as provided below, the contact end 32 is substantially planar and is spaced apart from the work surface 24. The circuit end 34 is configured to be in electrical communication with the pulse circuit 22.
The contact end 32 has a contact 32A. The contact 32A may be unitary with the contact end 32, or separately formed but attached thereto. The contact 32A may have the same width as the contact end 32 and extend along the contact end 32, as shown in
The contact 32A preferably extends upwardly from the contact end 32. The contact 32A may be at any location along the contact end 32 and, while only one contact 32A is shown in the Figures, there may be more than one. As shown in
The proximity conductor 18 is disposed in the terminal aperture 30 of the work surface 24. Additionally, as shown in
The proximity conductor 18 may be rigidly mounted with respect to the work surface 24 using any conventional coupling means. The proximity conductor 18 is electrically insulated from the first terminal 16 and the work surface 24. The proximity conductor 18 has a contact end 36, a circuit end 38, and a magnetic field generating portion 40.
The contact end 36 may be spaced apart from the work surface 24 and the circuit end 38. For example, there may be a gap of constant dimension between the contact end 36 and the work surface 24 or the gap may vary as it extends between the work surface 24 and the contact end 36.
The circuit end 38 is configured to be in electrical communication with the pulse circuit 22. Preferably, the proximity conductor 18 is unitarily formed, but it is understood the proximity conductor 18 may comprise a plurality of components in electrical communication with one another.
The magnetic field generating portion 40 and the contact end 36 extend at least partially to the circuit end 38 in an “L” shape; but it is understood the magnetic field generating portion 40 and the contact end 36 may form other shapes.
Near the work surface 24, the contact end 36 may have a reverse S-shape, as shown in
The magnetic field generating portion 40 extends transversely from the proximity conductor 18. In the preferred embodiment, the magnetic field generating portion 40 extends at approximately a 90 degree angle to the proximity conductor 18. The magnetic field generating portion 40 is cantilevered over the proximity conductor 18.
Opposite the connection of the magnetic field generating portion 40 to the proximity conductor 18, the contact 36A is located on the portion 40. The contact 36A may be unitary with the magnetic field generating portion 40, or separately formed but attached thereto.
The contact 36A preferably extends upwardly from the magnetic field generating portion 40. The contact 36A may be at any location along the magnetic field generating portion 40 and, while only one contact 36A is shown in the Figures, there may be more than one. As shown in
A preferred cross-sectional shape of the magnetic field generating portion 40, shown in
As shown in
The restraining member 20 as shown in
As shown schematically in
In use, the pulse welding system 10 is used to couple the second workpiece 14 to the first workpiece 12 using a pulse current delivered to one of the first terminal 16 or the proximity conductor 18 by the high current switch 52, as directed by one of an operator and a control system (not shown) of the pulse welding system 10.
Prior to application of the pulse current, the first workpiece 12 and the second workpiece 14 are secured between the restraining member 20 and the contacts 32A, 36A of the first terminal 16 and the proximity conductor 18, as shown in
The embossed portion 28 is spaced apart from the magnetic field generating portion 40 of the proximity conductor 18 with the insulator 41; however, it is understood an air gap may provide sufficient insulation. Simultaneously or after positioning of the second workpiece 14, the first workpiece 12 is abuttingly disposed against the substantially flat portion 26 of the second workpiece 14. More particularly, the lower surface 12B of the first workpiece 12 is placed in contact with the flat portion 26 of the upper surface 14A of the second workpiece. As shown in
Once the first workpiece 12 is disposed against the second workpiece 14 the restraining member 20, upon direction by the operator or the control system, is moved towards the work surface 24 until the restraining member 20 contacts the first workpiece 12. The control system may be configured to apply a predetermined amount of force to the first workpiece 12 with the restraining member 20 or the restraining member 20 may be configured to move a predetermined distance to restrain the first workpiece 12 and the second workpiece 14 between the contacts 32A, 36A and the restraining member 20. Restraining the first workpiece 12 and the second workpiece 14 between the contact 32A, 36A and the restraining member 20 causes the second workpiece 14 to be in electrical communication with the contact 32A of the first terminal 16 and the contact 36A of the proximity conductor 18. More particularly, contact 32A is located in direct physical contact with the lower surface 14B of one end of the second workpiece 14 and contact 36A is located in direct physical contact with the lower surface 14B of an opposite end of the second workpiece 14.
Upon direction by the operator or the control system, the capacitor bank 50 is charged using the inverter 48. Once a predetermined charge level is reached, as determined by the operator or the control system, the high current switch 52 is closed, delivering a pulse current to one of the first terminal 16 and the proximity conductor 18. The pulse current may have a range of amplitude from about 100 kA to about 300 kA. The pulse current travels through the first terminal 16, through the contact 32A, through the second workpiece 14 in a first direction through the contact 36A, and through the proximity conductor 18 in a second direction, as shown by the dashed lines in
The pulse current generates one or more magnetic fields between the proximity conductor 18 and the second workpiece 14, causing the rapid acceleration and collision of the embossed portion 28 of the second workpiece 14 with the first workpiece 12. Alternately, it is understood the pulse current may travel through the proximity conductor 18, the second workpiece 14, and through the first terminal 16. Magnetic pulse welding under such conditions may be referred to as “direct magnetic pulse welding,” as opposed to “inductive magnetic pulse welding,” where a workpiece to be formed does not form a portion of a magnetic pulse circuit.
As shown in
From
At least in part, the acceleration and direction of movement of the embossed portion 28 at an angle is due to the shape of the magnetic field generating portion 40 and may also be due to the location of the portion 40 relative to the embossed portion 28. As depicted in
A restraining member 20′ is provided that is the same as the member 20 except that it has a depression 48 formed therein. In
The first workpiece 12 may be formed according to the following steps. The restraining member 20′, upon direction by the operator or the control system, is moved towards the work surface 24 until the restraining member 20′ contacts the first workpiece 12. The control system may be configured to apply a predetermined amount of force to the first workpiece 12 with the restraining member 20′ or the restraining member 20 may be configured to move a predetermined distance to restrain the first workpiece 12 between the contacts 32A, 36A and the restraining member 20′. Restraining the first workpiece 12 between the contacts 32A, 36A and the restraining member 20′ causes the workpiece 12 to be in electrical communication with the contact 32A of the first terminal 16 and the contact 36A of the proximity conductor 18.
Contact 32A is located in direct physical contact with the lower surface 12B of one end of the first workpiece 12 and contact 36A is located in direct physical contact with the lower surface 12B of an opposite end of the first workpiece 12.
Upon direction by the operator or the control system, the capacitor bank 50 is charged using the inverter 48. Once a predetermined charge level is reached, as determined by the operator or the control system, the high current switch 52 is closed, delivering a pulse current to one of the first terminal 16 and the proximity conductor 18. The pulse current may have a range of amplitude from about 100 kA to about 300 kA. The pulse current travels through the first terminal 16, through the contact 32A, through the first workpiece 12 in a first direction through the contact 36A, and through the proximity conductor 18 in a second direction. The first and second directions are substantially opposite one another.
The pulse current generates one or more magnetic fields between the proximity conductor 18 and the first workpiece 12, causing the rapid acceleration of the first workpiece 12 adjacent the magnetic field generating portion 40 into the depression 48 of the restraining member 20′. The first workpiece 12 takes on the shape of the depression 48, as seen in
It can be readily appreciated that if the member 20′ had an outwardly extending portion, the first workpiece 12 would be similarly formed to comply with the shape of the outwardly extending portion.
The first flyer 54 has an upper surface 58, a lower surface 60, a planar portion 62 and an embossed portion 64. The planar portion 62, in the present embodiment, surrounds the embossed portion 64. The embossed portion 64 may have the features described above in the prior embodiments of the second workpiece 14. The lower surface 60 may be located in contact with the insulator 41, as shown in
The second flyer 56 has an upper surface 68, a lower surface 70, a planar portion 72 and an embossed portion 74. The planar portion 72, in the present embodiment, surrounds the embossed portion 74. The embossed portion 74 may have the features described above in the prior embodiments of the second workpiece 14. The lower surface 70 may be located in contact with the insulator 41, as shown in
The insulator 41 in
Edge portions 66, 76 of the fliers 54, 56, at the upstanding portion 78, may overlap one another such that one lies directly on top of the other. In the depicted embodiment, the first flyer 54 lies on top of the second flier 56, however, a vice versa orientation is also permissible.
The magnetic field generating portion 40 extends beneath the insulator 41. In the depicted embodiment, the portion 40 extends entirely along and beneath the embossed portions 64, 74.
Contact 32 contacts the planar portion 62 of the first flyer 54 and contact 36 contacts the planar portion 72 of the second flyer 56. It can be appreciated from the foregoing that the pulse current flows to contact 32, through flyer 54, through the overlap of flyer 54 to flyer 56, and to contact 36 in a first direction. The pulse current flows through portion 40 in a second direction, opposite the first direction, to create a magnetic field that drives the two embossed portions 64, 74 into the first workpiece 12.
The first workpiece 12 may be one or two pieces, if it is two pieces they may be connected to one another. The first workpiece 12 preferably extends entirely above the first and second fliers 54, 56.
The process described above may be used to move the second workpiece 14 into contact with the first workpiece 12, while the structure 80 is located therebetween. As can be appreciated from
If the structure 80 and either or both of the first or second workpieces 12, 14 would not normally be paired together due to galvanic corrosion, the structure 80 and the first and/or second workpieces 12, 14 could be isolated from one another by an insulator, such as a dielectric coating.
A welding process as described above may be used to drive the second workpiece 14, and thus the structure 80′, into secure contact with the first workpiece 12, such as by welding each of them to one another. It is also permissible for the second workpiece 14 to be formed about the structure 80′ and welded to the first workpiece 12 to secure them together.
In the depicted embodiment, the first and third sections 82, 86 are depicted as parallel to one another, but they need not be. The second section 84 may connect the first and third sections 82, 86 together. In the depicted embodiment, the second section 84 may be angled with respect to the first and third sections 82, 86. The first workpiece 12′ may be supported by a restraining member 20′. The support may come from the restraining member 20′ having a shape that is the same as, or that approximates, the first workpiece 12′.
The second workpiece 14′ may have a shape that approximates the first workpiece 12′, as shown in
The contact 32 is located into electrical contact with the first section 82. An insulator 41′ is located between the second workpiece 14′ and a magnetic field generating portion 40′. The insulator 41′ has a shape that approximates the shape of the second workpiece 14′ or which may the same. A contact 36 is located in electrical contact with third section 86.
The magnetic field generating portion 40′ extends from the contact 36 beneath the insulator 41′. The portion 40′ may have a shape complimentary to the shape of the second workpiece 14′.
A pulse current is delivered to contact 32, where it travels through second workpiece 14′ and through contact 36. The current travels through the portion 40′ in a direction that is opposite, or substantially opposite, its direction through the second workpiece 14′. The opposite direction currents create a magnetic field that drives the second workpiece 14′ into the first workpiece 12′ to weld them together as shown in
The sensor 88 may be for any application, such as for acoustics, sound or vibration, chemical, electric, magnetic or radio, moisture or humidity, flow or fluid velocity, position, angle, displacement, distance, speed or acceleration, optical, light or imaging, pressure, force, density, thermal, heat or temperature.
In one embodiment, the sensor 88 may be such as a voltage monitoring sensor that may be used located between the two workpieces 12,14, which may be battery plates. Some sensors, such as voltage monitoring sensors, prefer to remain motionless. By locating a voltage monitoring sensor at least partially in the weld area 90, the sensor remains fixed in position. The sensor 88 may also be such as a thermocouple.
The figures depict a wire 92 extending from the sensor 88 and through the workpieces 12, 14. The location and orientation of the wire 92 is not limited to what is depicted in the figures. Instead, the wire 92 may extend from any location or orientation and there may be more than one wire.
The wire 92 may be such as a communication wire that permits the sensor 88 to communicate with a data collection device (not shown), such as a computer. Communications may be sent to the sensor 88 along the wire 92, and communications may be sent from the sensor 88 to the data collection device.
Alternatively, or additionally, the sensor 88 may be capable of communicating with the data collection device wirelessly. It can be appreciated that in that instance, a wire may not be required, particularly where the workpieces 12, 14 were comprised of nonmagnetic materials. The sensor 88 can be entirely surrounded by and enclosed within the weld area 90 such that fluid cannot come into or out of the area where the sensor 88 is located.
In accordance with the provisions of the patent statutes, the present invention has been described in what is considered to represent its preferred embodiments. However, it should be noted that the invention can be practiced otherwise than as specifically illustrated and described without departing from its spirit or scope.
Yablochnikov, Boris A., O'Neil, Tom, Steigerwalt, Eve S., Kummerow, Jack A.
Patent | Priority | Assignee | Title |
10017971, | Oct 22 2013 | Whirlpool Corporation | Method of making an appliance cabinet |
Patent | Priority | Assignee | Title |
3140539, | |||
3520049, | |||
3591757, | |||
3794805, | |||
3851139, | |||
3947290, | Nov 23 1973 | General Motors Corporation | Process and apparatus for making intercell connectors by an extrusion-fusion technique |
4055291, | Dec 15 1975 | ELECTRODE CORPORATION, A CORP OF DE | Explosion bonding of bipolar electrode backplates |
4234776, | Jul 12 1978 | Thermatool Corp. | Method of producing areas of alloy metal on a metal part using electric currents |
4916278, | Sep 01 1989 | Thermatool Corporation | Severing metal strip with high frequency electrical current |
6255631, | Nov 29 1999 | METALSA S A DE C V | Apparatus and method for joining vehicle frame components |
6340053, | Feb 05 1999 | Dana Canada Corporation | Self-enclosing heat exchanger with crimped turbulizer |
6513240, | Jun 02 1998 | Method of forming a heat exchanger stack | |
6523876, | Sep 30 2001 | METALSA S A DE C V | Unitary cross member and body mount support bracket for a vehicle body and frame assembly |
6531688, | Jun 20 1997 | Dana Automotive Systems Group, LLC | Method of magnetic pulse welding an end fitting to a driveshaft tube of a vehicular driveshaft |
6548792, | Jun 16 1995 | METALSA S A DE C V | Molecular bonding of vehicle frame components using magnetic impulse welding techniques |
6561722, | Jan 14 2000 | FUEL CELL COMPONENTS AND INTEGRATORS, INC | Method of fabricating structural joints |
6772934, | Oct 11 2002 | Dynamic Materials Corporation | Kinetic energy welding process |
6910617, | Mar 06 2002 | Dana Automotive Systems Group, LLC | Method for securing a yoke to a tube using magnetic pulse welding techniques |
7076981, | Mar 30 2004 | GM Global Technology Operations LLC | Electromagnetic formation of fuel cell plates |
7959057, | Mar 31 2005 | RENAULT S A S | Tool and method for assembling metal parts by impacting with the aid of a magnetic force using two electromagnetic coils movable with respect to each other |
20020097549, | |||
20050229377, | |||
20060131300, | |||
20060156776, | |||
20080120844, | |||
20100059254, | |||
20100140328, | |||
DE102010052457, | |||
EP1935551, | |||
JP200011964, | |||
JP2003260569, | |||
JP200434155, | |||
JP2006088172, | |||
JP200688172, | |||
JP2010110814, | |||
JP201179036, | |||
JP53131254, | |||
JP5586690, | |||
JP64020985, | |||
SU518898, | |||
WO2008104668, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Oct 09 2012 | Dana Automotive Systems Group, LLC | (assignment on the face of the patent) | / | |||
Oct 15 2012 | STEIGERWALT, EVE S | Dana Automotive Systems Group, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 029164 | /0296 | |
Oct 19 2012 | KUMMEROW, JACK A C , II | Dana Automotive Systems Group, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 029164 | /0296 | |
Oct 22 2012 | O NEIL, TOM | Dana Automotive Systems Group, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 029164 | /0296 | |
Apr 16 2020 | Dana Automotive Systems Group, LLC | CITIBANK, N A | SECURITY AGREEMENT BRIDGE | 052459 | /0001 | |
Apr 16 2020 | Dana Heavy Vehicle Systems Group, LLC | CITIBANK, N A | SECURITY AGREEMENT BRIDGE | 052459 | /0001 | |
Apr 16 2020 | FAIRFIELD MANUFACTURING COMPANY, INC | CITIBANK, N A | SECURITY AGREEMENT SUPPLEMENT | 052459 | /0224 | |
Apr 16 2020 | Dana Limited | CITIBANK, N A | SECURITY AGREEMENT BRIDGE | 052459 | /0001 | |
Apr 16 2020 | Dana Automotive Systems Group, LLC | CITIBANK, N A | SECURITY AGREEMENT SUPPLEMENT | 052459 | /0224 | |
Apr 16 2020 | Dana Limited | CITIBANK, N A | SECURITY AGREEMENT SUPPLEMENT | 052459 | /0224 | |
Apr 16 2020 | Dana Heavy Vehicle Systems Group, LLC | CITIBANK, N A | SECURITY AGREEMENT SUPPLEMENT | 052459 | /0224 | |
Apr 16 2020 | FAIRFIELD MANUFACTURING COMPANY, INC | CITIBANK, N A | SECURITY AGREEMENT BRIDGE | 052459 | /0001 | |
Jun 19 2020 | CITIBANK, N A | Dana Automotive Systems Group, LLC | RELEASE BY SECURED PARTY SEE DOCUMENT FOR DETAILS | 053309 | /0686 | |
Jun 19 2020 | CITIBANK, N A | Dana Limited | RELEASE BY SECURED PARTY SEE DOCUMENT FOR DETAILS | 053309 | /0686 | |
Jun 19 2020 | CITIBANK, N A | FAIRFIELD MANUFACTURING COMPANY, INC | RELEASE BY SECURED PARTY SEE DOCUMENT FOR DETAILS | 053309 | /0686 | |
Jun 19 2020 | CITIBANK, N A | Dana Heavy Vehicle Systems Group, LLC | RELEASE BY SECURED PARTY SEE DOCUMENT FOR DETAILS | 053309 | /0686 |
Date | Maintenance Fee Events |
Jun 04 2018 | M1551: Payment of Maintenance Fee, 4th Year, Large Entity. |
May 18 2022 | M1552: Payment of Maintenance Fee, 8th Year, Large Entity. |
Date | Maintenance Schedule |
Dec 02 2017 | 4 years fee payment window open |
Jun 02 2018 | 6 months grace period start (w surcharge) |
Dec 02 2018 | patent expiry (for year 4) |
Dec 02 2020 | 2 years to revive unintentionally abandoned end. (for year 4) |
Dec 02 2021 | 8 years fee payment window open |
Jun 02 2022 | 6 months grace period start (w surcharge) |
Dec 02 2022 | patent expiry (for year 8) |
Dec 02 2024 | 2 years to revive unintentionally abandoned end. (for year 8) |
Dec 02 2025 | 12 years fee payment window open |
Jun 02 2026 | 6 months grace period start (w surcharge) |
Dec 02 2026 | patent expiry (for year 12) |
Dec 02 2028 | 2 years to revive unintentionally abandoned end. (for year 12) |